- •Textbook Series
- •Contents
- •1 Overview and Definitions
- •Overview
- •General Definitions
- •Glossary
- •List of Symbols
- •Greek Symbols
- •Others
- •Self-assessment Questions
- •Answers
- •2 The Atmosphere
- •Introduction
- •The Physical Properties of Air
- •Static Pressure
- •Temperature
- •Air Density
- •International Standard Atmosphere (ISA)
- •Dynamic Pressure
- •Key Facts
- •Measuring Dynamic Pressure
- •Relationships between Airspeeds
- •Airspeed
- •Errors and Corrections
- •V Speeds
- •Summary
- •Questions
- •Answers
- •3 Basic Aerodynamic Theory
- •The Principle of Continuity
- •Bernoulli’s Theorem
- •Streamlines and the Streamtube
- •Summary
- •Questions
- •Answers
- •4 Subsonic Airflow
- •Aerofoil Terminology
- •Basics about Airflow
- •Two Dimensional Airflow
- •Summary
- •Questions
- •Answers
- •5 Lift
- •Aerodynamic Force Coefficient
- •The Basic Lift Equation
- •Review:
- •The Lift Curve
- •Interpretation of the Lift Curve
- •Density Altitude
- •Aerofoil Section Lift Characteristics
- •Introduction to Drag Characteristics
- •Lift/Drag Ratio
- •Effect of Aircraft Weight on Minimum Flight Speed
- •Condition of the Surface
- •Flight at High Lift Conditions
- •Three Dimensional Airflow
- •Wing Terminology
- •Wing Tip Vortices
- •Wake Turbulence: (Ref: AIC P 072/2010)
- •Ground Effect
- •Conclusion
- •Summary
- •Answers from page 77
- •Answers from page 78
- •Questions
- •Answers
- •6 Drag
- •Introduction
- •Parasite Drag
- •Induced Drag
- •Methods of Reducing Induced Drag
- •Effect of Lift on Parasite Drag
- •Aeroplane Total Drag
- •The Effect of Aircraft Gross Weight on Total Drag
- •The Effect of Altitude on Total Drag
- •The Effect of Configuration on Total Drag
- •Speed Stability
- •Power Required (Introduction)
- •Summary
- •Questions
- •Annex C
- •Answers
- •7 Stalling
- •Introduction
- •Cause of the Stall
- •The Lift Curve
- •Stall Recovery
- •Aircraft Behaviour Close to the Stall
- •Use of Flight Controls Close to the Stall
- •Stall Recognition
- •Stall Speed
- •Stall Warning
- •Artificial Stall Warning Devices
- •Basic Stall Requirements (EASA and FAR)
- •Wing Design Characteristics
- •The Effect of Aerofoil Section
- •The Effect of Wing Planform
- •Key Facts 1
- •Super Stall (Deep Stall)
- •Factors that Affect Stall Speed
- •1g Stall Speed
- •Effect of Weight Change on Stall Speed
- •Composition and Resolution of Forces
- •Using Trigonometry to Resolve Forces
- •Lift Increase in a Level Turn
- •Effect of Load Factor on Stall Speed
- •Effect of High Lift Devices on Stall Speed
- •Effect of CG Position on Stall Speed
- •Effect of Landing Gear on the Stall Speed
- •Effect of Engine Power on Stall Speed
- •Effect of Mach Number (Compressibility) on Stall Speed
- •Effect of Wing Contamination on Stall Speed
- •Warning to the Pilot of Icing-induced Stalls
- •Stabilizer Stall Due to Ice
- •Effect of Heavy Rain on Stall Speed
- •Stall and Recovery Characteristics of Canards
- •Spinning
- •Primary Causes of a Spin
- •Phases of a Spin
- •The Effect of Mass and Balance on Spins
- •Spin Recovery
- •Special Phenomena of Stall
- •High Speed Buffet (Shock Stall)
- •Answers to Questions on Page 173
- •Key Facts 2
- •Questions
- •Key Facts 1 (Completed)
- •Key Facts 2 (Completed)
- •Answers
- •8 High Lift Devices
- •Purpose of High Lift Devices
- •Take-off and Landing Speeds
- •Augmentation
- •Flaps
- •Trailing Edge Flaps
- •Plain Flap
- •Split Flap
- •Slotted and Multiple Slotted Flaps
- •The Fowler Flap
- •Comparison of Trailing Edge Flaps
- •and Stalling Angle
- •Drag
- •Lift / Drag Ratio
- •Pitching Moment
- •Centre of Pressure Movement
- •Change of Downwash
- •Overall Pitch Change
- •Aircraft Attitude with Flaps Lowered
- •Leading Edge High Lift Devices
- •Leading Edge Flaps
- •Effect of Leading Edge Flaps on Lift
- •Leading Edge Slots
- •Leading Edge Slat
- •Automatic Slots
- •Disadvantages of the Slot
- •Drag and Pitching Moment of Leading Edge Devices
- •Trailing Edge Plus Leading Edge Devices
- •Sequence of Operation
- •Asymmetry of High Lift Devices
- •Flap Load Relief System
- •Choice of Flap Setting for Take-off, Climb and Landing
- •Management of High Lift Devices
- •Flap Extension Prior to Landing
- •Questions
- •Annexes
- •Answers
- •9 Airframe Contamination
- •Introduction
- •Types of Contamination
- •Effect of Frost and Ice on the Aircraft
- •Effect on Instruments
- •Effect on Controls
- •Water Contamination
- •Airframe Aging
- •Questions
- •Answers
- •10 Stability and Control
- •Introduction
- •Static Stability
- •Aeroplane Reference Axes
- •Static Longitudinal Stability
- •Neutral Point
- •Static Margin
- •Trim and Controllability
- •Key Facts 1
- •Graphic Presentation of Static Longitudinal Stability
- •Contribution of the Component Surfaces
- •Power-off Stability
- •Effect of CG Position
- •Power Effects
- •High Lift Devices
- •Control Force Stability
- •Manoeuvre Stability
- •Stick Force Per ‘g’
- •Tailoring Control Forces
- •Longitudinal Control
- •Manoeuvring Control Requirement
- •Take-off Control Requirement
- •Landing Control Requirement
- •Dynamic Stability
- •Longitudinal Dynamic Stability
- •Long Period Oscillation (Phugoid)
- •Short Period Oscillation
- •Directional Stability and Control
- •Sideslip Angle
- •Static Directional Stability
- •Contribution of the Aeroplane Components.
- •Lateral Stability and Control
- •Static Lateral Stability
- •Contribution of the Aeroplane Components
- •Lateral Dynamic Effects
- •Spiral Divergence
- •Dutch Roll
- •Pilot Induced Oscillation (PIO)
- •High Mach Numbers
- •Mach Trim
- •Key Facts 2
- •Summary
- •Questions
- •Key Facts 1 (Completed)
- •Key Facts 2 (Completed)
- •Answers
- •11 Controls
- •Introduction
- •Hinge Moments
- •Control Balancing
- •Mass Balance
- •Longitudinal Control
- •Lateral Control
- •Speed Brakes
- •Directional Control
- •Secondary Effects of Controls
- •Trimming
- •Questions
- •Answers
- •12 Flight Mechanics
- •Introduction
- •Straight Horizontal Steady Flight
- •Tailplane and Elevator
- •Balance of Forces
- •Straight Steady Climb
- •Climb Angle
- •Effect of Weight, Altitude and Temperature.
- •Power-on Descent
- •Emergency Descent
- •Glide
- •Rate of Descent in the Glide
- •Turning
- •Flight with Asymmetric Thrust
- •Summary of Minimum Control Speeds
- •Questions
- •Answers
- •13 High Speed Flight
- •Introduction
- •Speed of Sound
- •Mach Number
- •Effect on Mach Number of Climbing at a Constant IAS
- •Variation of TAS with Altitude at a Constant Mach Number
- •Influence of Temperature on Mach Number at a Constant Flight Level and IAS
- •Subdivisions of Aerodynamic Flow
- •Propagation of Pressure Waves
- •Normal Shock Waves
- •Critical Mach Number
- •Pressure Distribution at Transonic Mach Numbers
- •Properties of a Normal Shock Wave
- •Oblique Shock Waves
- •Effects of Shock Wave Formation
- •Buffet
- •Factors Which Affect the Buffet Boundaries
- •The Buffet Margin
- •Use of the Buffet Onset Chart
- •Delaying or Reducing the Effects of Compressibility
- •Aerodynamic Heating
- •Mach Angle
- •Mach Cone
- •Area (Zone) of Influence
- •Bow Wave
- •Expansion Waves
- •Sonic Bang
- •Methods of Improving Control at Transonic Speeds
- •Questions
- •Answers
- •14 Limitations
- •Operating Limit Speeds
- •Loads and Safety Factors
- •Loads on the Structure
- •Load Factor
- •Boundary
- •Design Manoeuvring Speed, V
- •Effect of Altitude on V
- •Effect of Aircraft Weight on V
- •Design Cruising Speed V
- •Design Dive Speed V
- •Negative Load Factors
- •The Negative Stall
- •Manoeuvre Boundaries
- •Operational Speed Limits
- •Gust Loads
- •Effect of a Vertical Gust on the Load Factor
- •Effect of the Gust on Stalling
- •Operational Rough-air Speed (V
- •Landing Gear Speed Limitations
- •Flap Speed Limit
- •Aeroelasticity (Aeroelastic Coupling)
- •Flutter
- •Control Surface Flutter
- •Aileron Reversal
- •Questions
- •Answers
- •15 Windshear
- •Introduction (Ref: AIC 84/2008)
- •Microburst
- •Windshear Encounter during Approach
- •Effects of Windshear
- •“Typical” Recovery from Windshear
- •Windshear Reporting
- •Visual Clues
- •Conclusions
- •Questions
- •Answers
- •16 Propellers
- •Introduction
- •Definitions
- •Aerodynamic Forces on the Propeller
- •Thrust
- •Centrifugal Twisting Moment (CTM)
- •Propeller Efficiency
- •Variable Pitch Propellers
- •Power Absorption
- •Moments and Forces Generated by a Propeller
- •Effect of Atmospheric Conditions
- •Questions
- •Answers
- •17 Revision Questions
- •Questions
- •Answers
- •Explanations to Specimen Questions
- •Specimen Examination Paper
- •Answers to Specimen Exam Paper
- •Explanations to Specimen Exam Paper
- •18 Index
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Overview and Definitions |
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Definitions and Overview 1
List of Symbols
The following symbols are used throughout these notes. However, no universal defining standard for their use exists. Other books on the subject may use some of these symbols with different definitions. Every effort has been made to employ symbols that are widely accepted and that conform to the Learning Objectives.
a |
speed of sound |
AC |
aerodynamic centre |
AR |
aspect ratio |
b |
span |
C |
Centigrade |
c |
chord length |
CD |
drag coefficient |
CG |
centre of gravity |
CP |
centre of pressure |
CL |
lift coefficient |
CM |
pitching moment coefficient |
D |
drag |
Di |
induced drag |
F |
force |
g |
acceleration due to gravity, also used for load factor |
KKelvin
Llift
L/D |
lift to drag ratio |
M |
Mach number |
mmass
nload factor
p pressure
Q or q dynamic pressure
Sarea; wing area
Ttemperature
t/c |
thickness-chord ratio |
V |
free stream speed (TAS) |
VS |
stall speed |
W |
weight |
Greek Symbols
α (alpha) angle of attack
β(beta) sideslip angle
γ(gamma) angle of climb or descent (delta) increment in
μ (mu) Mach angle
ρ(rho) density
σ (sigma) relative density
φ(phi) angle of bank
14
Overview and Definitions |
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Others
proportional to
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= is approximately equal to
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Note: The Greek symbol γ (gamma) has been used in these notes to denote angle of climb and descent. The Learning Objectives use θ (theta). Evidence exists that a question in the exam uses γ (gamma) for angle of climb and descent. The notes have been amended to use γ, but consider either γ or θ to indicate angle of climb and descent.
Overview and Definitions 1
15
1 Questions
Questions 1
Self-assessment Questions
Aircraft (1)
Mass: 2000 kilograms (kg)
Engine thrust: 4000 newtons (N)
V1 speed: 65 knots (kt)
Take-off run to reach V1: 750 metres (m)
Time taken to reach V1: 30 seconds (s)
Aircraft (2)
Mass: 2000 kilograms (kg)
Engine thrust: 8000 newtons (N)
V1 speed: 130 knots (kt)
Take-off run to reach V1: 1500 metres (m)
Time taken to reach V1: 40 seconds (s)
where 1 nautical mile = 6080 ft and 1 metre = 3.28 ft
At V1 both aircraft experience an engine failure and take-off is abandoned.
a.How much work was done to aircraft (1) getting to V1?
b.How much power was used to get aircraft (1) to V1?
c.How much work was done to aircraft (2) getting to V1?
d.How much power was used to get aircraft (2) to V1?
e.How much momentum does aircraft (1) possess at V1?
f.How much momentum does aircraft (2) possess at V1?
g.How many times greater is the momentum of aircraft (2)?
h.How much kinetic energy does aircraft (1) possess at V1?
i.How much kinetic energy does aircraft (2) possess at V1?
j.How many times greater is the kinetic energy of aircraft (2)?
k.State the mass and velocity relationship of both aircraft and compare to their momentum and kinetic energy.
l.Which has the greater effect on kinetic energy, mass or velocity?
m.What must be done with the kinetic energy so the aircraft can be brought to a stop?
16
Questions 1
1.An aircraft’s mass is a result of:
a.its weight.
b.how big it is.
c.how much matter it contains.
d.its volume.
2.The unit of mass is the:
a.joule.
b.watt.
c.newton.
d.kilogram.
3.The definition of a force is:
a.that which causes a reaction to take place.
b.thrust and drag only.
c.a push or a pull.
d.the result of an applied input.
4.The unit of force is the:
a.mass-kilogram.
b.newton-metre.
c.joule.
d.newton.
5.The unit of weight is the:
a.kilogram.
b.newton.
c.watt.
d.kilowatt.
6.Weight is the result of:
a.the force on mass due to gravity.
b.the action of a falling mass.
c.how much matter the object contains.
d.the rate of mass per unit area.
7.About which point does an aircraft rotate?
a.The wings.
b.The main undercarriage.
c.The centre of gravity.
d.The rudder.
8.If a force is applied to a mass and the mass does not move:
a.work is done even though there is no movement of the mass.
b.work is done only if the mass moves a long way.
c.power is exerted, but no work is done.
d.no work is done.
Questions 1
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The unit of work is called the: |
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pascal. |
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joule. |
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c. |
watt. |
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d. |
kilogram. |
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10. |
The unit of power is called the: |
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joule. |
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newton-metre. |
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c. |
watt. |
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d. |
metre per second. |
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11. |
If a force of 20 newtons moves a mass 5 metres: |
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1 - the work done is 100 Nm |
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2 - the work done is 100 joules |
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3 - the work done is 4 joules |
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4 - the work done is 0.25 joules |
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The correct statements are: |
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1 only. |
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1 and 3. |
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c. |
1 and 2. |
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d. |
2 only. |
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12. |
If a force of 50 newtons is applied to a 10 kg mass and the mass moves 10 metres |
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and a force of 50 newtons is applied to a 100 kg mass which moves 10 metres: |
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the work done is the same in both cases. |
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less work is done to the 10 kg mass. |
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c. |
more work is done to the 10 kg mass. |
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d. |
more work is done to the 100 kg mass. |
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13. |
The definition of power is: |
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the rate of force applied. |
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the rate of movement per second. |
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c. |
the rate of doing work. |
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d. |
the rate of applied force. |
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14. |
If a force of 500 newtons moves a mass 1000 metres in 2 mins, the power used is: |
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4167 watts. |
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b. |
250 kilowatts. |
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c. |
1 megawatt. |
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d. |
4 watts. |
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15. |
Kinetic energy is: |
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the energy a mass possesses due to its position in space. |
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the energy a mass possesses when a force has been applied. |
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the energy a mass possesses due to the force of gravity. |
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d. |
the energy a mass possesses because of its motion. |
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16. |
The unit of kinetic energy is the: |
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joule. |
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b. |
metre per second. |
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watt. |
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d. |
newton-metre per second. |
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17. |
When considering kinetic energy: |
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- a moving mass can apply a force by being brought to rest. |
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- kinetic energy is the energy possessed by a body because of its motion. |
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- if a body’s kinetic energy is increased, a force must have been applied. |
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- kinetic energy = ½ m V2 joules. |
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The combination of correct statements is: |
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1 and 2. |
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1, 2, 3 and 4. |
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4 only. |
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d. |
2 and 4. |
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18. |
The property of inertia is said to be: |
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the energy possessed by a body because of its motion. |
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the opposition which a body offers to a change in motion. |
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that every action has an equal and opposite reaction. |
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d. |
the quantity of motion possessed by a body. |
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19. |
Considering Newton’s first law of motion: |
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- a body is said to have energy if it has the ability to do work. |
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- the amount of energy a body possesses is measured by the amount of work it |
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can do. |
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3 |
- a body will tend to remain at rest, or in uniform motion in a straight line, unless |
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acted upon by an external force. |
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4 |
- to move a stationary object or to make a moving object change its direction, a |
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force must be applied. |
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The combination with the correct statements is: |
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3 and 4. |
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3 only. |
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1 and 2. |
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d. |
1, 2, 3 and 4. |
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20. |
Considering Newton’s second law of motion: |
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1 - every action has an equal and opposite reaction. |
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2 - if the same force is applied, the larger the mass the slower the acceleration. |
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3 - if two forces are applied to the same mass, the bigger the force the greater the |
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acceleration. |
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4 - the acceleration of a body from a state of rest, or uniform motion in a straight |
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line, is proportional to the applied force and inversely proportional to the mass. |
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The combination of true statements is: |
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1 only. |
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1, 2, 3 and 4. |
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c. |
2, 3, and 4. |
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d. |
3 and 4. |
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21. |
Newton’s third law of motion states: |
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the energy possessed by a mass is inversely proportional to its velocity. |
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b. |
every force has an equal and opposite inertia. |
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c. |
for every force there is an action. |
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d. |
every action has an equal and opposite reaction. |
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22. |
The definition of velocity is the: |
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a. |
rate of change of acceleration. |
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b. |
rate of change of displacement. |
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c. |
the quantity of motion possessed by a body. |
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d. |
the acceleration of a body in direct proportion to its mass. |
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23. |
When considering acceleration: |
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1 - acceleration is the rate of change of velocity. |
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2 - the units of acceleration are metres per second. |
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3 - the units of acceleration are kilogram-metres per second. |
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4 - the units of acceleration are seconds per metre per metre. |
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The combination of correct statements is: |
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a. |
4 only. |
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b. |
1 and 4. |
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c. |
1 only. |
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d. |
1 and 2. |
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24. |
The definition of momentum is: |
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a. |
the quantity of mass possessed by a body. |
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b. |
the quantity of inertia possessed by a body. |
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c. |
the quantity of motion possessed by a body. |
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d. |
the opposition which a body offers to a change in velocity. |
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25. |
A force of 24 newtons moves a 10 kg mass 60 metres in 1 minute. The power used |
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Questions |
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- 24 watts. |
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2 |
- 240 watts. |
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- force times distance moved in one second. |
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- force times the distance the mass is moved in one second. |
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Which of the preceding statements are correct: |
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a. |
1 and 3. |
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b. |
1, 3 and 4. |
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c. |
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2 and 4. |
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d. |
4 only. |
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26. |
When considering momentum: |
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1 |
- momentum is the quantity of motion possessed by a body. |
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2 |
- momentum is the tendency of a body to continue in motion after being placed |
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in motion. |
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3 |
- a mass of 2000 kg moving at 55 m/s has 110 000 kg-m/s of momentum. |
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4 |
- a large mass moving at 50 m/s will have less momentum than a small mass |
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moving at 50 m/s. |
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The correct combination of statements is: |
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a. |
1 and 3. |
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b. |
1, 2, 3 and 4. |
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c. |
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1, 2 and 3. |
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d. |
2, 3 and 4. |
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